Simulation of hypersonic shock wave laminar boundary layer interaction on hollow cylinder flare

Nadia Kianvashrad, Doyle Knight

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Scopus citations

Abstract

Hypersonic high enthalpy laminar flow over a 30◦ hollow cylinder flare is simulated using the GASP and GASPex software. The simulations are based on the experiments performed in the LENS-XX wind tunnel at the Calspan-University of Buffalo Research Center (CUBRC). The total enthalpy varies from 5.07 to 21.85 M J/kg. Simulations are performed using both the Park I and perfect gas models. Steady-state solutions obtained by Gauss-Seidel iteration and time-accurate integration are compared. Grid convergence of the simulations is shown. The heat transfer and pressure on the isothermal cold wall are compared with experimental data.

Original languageEnglish (US)
Title of host publication54th AIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103933
DOIs
StatePublished - 2016
Event54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States
Duration: Jan 4 2016Jan 8 2016

Publication series

Name54th AIAA Aerospace Sciences Meeting
Volume0

Other

Other54th AIAA Aerospace Sciences Meeting, 2016
CountryUnited States
CitySan Diego
Period1/4/161/8/16

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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